GB2547049B - Integrated heater - Google Patents
Integrated heaterInfo
- Publication number
- GB2547049B GB2547049B GB201602240A GB201602240A GB2547049B GB 2547049 B GB2547049 B GB 2547049B GB 201602240 A GB201602240 A GB 201602240A GB 201602240 A GB201602240 A GB 201602240A GB 2547049 B GB2547049 B GB 2547049B
- Authority
- GB
- United Kingdom
- Prior art keywords
- integrated heater
- heater
- integrated
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
- B32B3/266—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/047—Heating to prevent icing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
- F02K1/82—Jet pipe walls, e.g. liners
- F02K1/827—Sound absorbing structures or liners
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B3/00—Ohmic-resistance heating
- H05B3/40—Heating elements having the shape of rods or tubes
- H05B3/42—Heating elements having the shape of rods or tubes non-flexible
- H05B3/48—Heating elements having the shape of rods or tubes non-flexible heating conductor embedded in insulating material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/10—Properties of the layers or laminate having particular acoustical properties
- B32B2307/102—Insulating
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0206—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
- F05D2260/962—Preventing, counteracting or reducing vibration or noise by means of "anti-noise"
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
- F05D2260/963—Preventing, counteracting or reducing vibration or noise by Helmholtz resonators
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
- Soundproofing, Sound Blocking, And Sound Damping (AREA)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB201602240A GB2547049B (en) | 2016-02-08 | 2016-02-08 | Integrated heater |
US16/074,442 US11338933B2 (en) | 2016-02-08 | 2017-02-08 | Acoustic honeycomb panel with integrated electrical heater |
EP17705458.2A EP3414446B1 (en) | 2016-02-08 | 2017-02-08 | Acoustic honeycomb panel with integrated electrical heater |
PCT/GB2017/050312 WO2017137740A1 (en) | 2016-02-08 | 2017-02-08 | Acoustic honeycomb panel with integrated electrical heater |
CN201780010410.6A CN109072816B (en) | 2016-02-08 | 2017-02-08 | Acoustic honeycomb panel with integrated electric heater |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB201602240A GB2547049B (en) | 2016-02-08 | 2016-02-08 | Integrated heater |
Publications (3)
Publication Number | Publication Date |
---|---|
GB201602240D0 GB201602240D0 (en) | 2016-03-23 |
GB2547049A GB2547049A (en) | 2017-08-09 |
GB2547049B true GB2547049B (en) | 2019-12-25 |
Family
ID=55641976
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB201602240A Active GB2547049B (en) | 2016-02-08 | 2016-02-08 | Integrated heater |
Country Status (5)
Country | Link |
---|---|
US (1) | US11338933B2 (en) |
EP (1) | EP3414446B1 (en) |
CN (1) | CN109072816B (en) |
GB (1) | GB2547049B (en) |
WO (1) | WO2017137740A1 (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10708979B2 (en) | 2016-10-07 | 2020-07-07 | De-Ice Technologies | Heating a bulk medium |
US10494107B2 (en) * | 2017-01-03 | 2019-12-03 | Goodrich Corporation | Additive manufacturing of conformal deicing and boundary layer control surface for aircraft |
FR3070674B1 (en) | 2017-09-06 | 2019-09-13 | Safran Nacelles | INTEGRATION WITH ACOUSTIC LEVER DEGIVREE |
GB201720603D0 (en) | 2017-12-11 | 2018-01-24 | Rolls Royce Plc | Fairings for power generation machines |
GB201802768D0 (en) | 2018-02-21 | 2018-04-04 | Rolls Royce Plc | Fairings for power generation machines |
CA3110343A1 (en) | 2018-08-27 | 2020-03-05 | De-Ice Technologies, Inc. | De-icing systems |
FR3085437B1 (en) | 2018-09-05 | 2020-11-20 | Airbus Operations Sas | AIR INTAKE STRUCTURE OF AN AIRCRAFT NACELLE |
CN212899157U (en) | 2020-07-27 | 2021-04-06 | 开利公司 | Noise reduction device for fan outlet side and heat exchange system comprising same |
FR3116642A1 (en) * | 2020-11-24 | 2022-05-27 | Airbus Operations | Resistive skin shell incorporating perforated metal strips, and acoustic internal wall of an aircraft air intake formed from such resistive skin shells. |
CN112629807B (en) * | 2021-03-09 | 2022-01-11 | 中国空气动力研究与发展中心低速空气动力研究所 | Method for removing ice growing on surface of silk thread hot knife and model |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5841079A (en) * | 1997-11-03 | 1998-11-24 | Northrop Grumman Corporation | Combined acoustic and anti-ice engine inlet liner |
EP1845018A2 (en) * | 2006-04-14 | 2007-10-17 | Rohr, Inc. | Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein |
EP2292514A2 (en) * | 2009-09-03 | 2011-03-09 | The Boeing Company | Ice protection system and method |
GB2476855A (en) * | 2009-11-27 | 2011-07-13 | Rolls Royce Plc | Acoustic liner and heat exchanger for gas turbine inlet duct |
WO2014102682A1 (en) * | 2012-12-27 | 2014-07-03 | Alenia Aermacchi S.Pa. | Nacelle for aircraft, provided with a built-in system for anti-icing protection and acoustic absorption |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4743740A (en) * | 1985-10-07 | 1988-05-10 | Rohr Industries, Inc. | Buried element deicer |
US7291815B2 (en) | 2006-02-24 | 2007-11-06 | Goodrich Corporation | Composite ice protection heater and method of producing same |
FR2908737B1 (en) * | 2006-11-16 | 2009-12-04 | Airbus France | ACOUSTIC COATING FOR AIRCRAFT INCORPORATING A JELLY EFFECT FROST TREATMENT SYSTEM. |
US20080166563A1 (en) * | 2007-01-04 | 2008-07-10 | Goodrich Corporation | Electrothermal heater made from thermally conducting electrically insulating polymer material |
FR2928625B1 (en) * | 2008-03-14 | 2012-11-30 | Aircelle Sa | ELECTRIC DEFROSTING DEVICE |
WO2009117408A1 (en) * | 2008-03-18 | 2009-09-24 | Watlow Electric Manufacturing Company | Layered heater system with honeycomb core structure |
US9469408B1 (en) * | 2009-09-03 | 2016-10-18 | The Boeing Company | Ice protection system and method |
GB0920741D0 (en) * | 2009-11-27 | 2010-01-13 | Rolls Royce Plc | Air flow passage liner |
FR3024124B1 (en) * | 2014-07-22 | 2018-03-02 | Safran Nacelles | METHOD FOR SETTING A DEFROSTING SYSTEM ON AN AIRCRAFT COMPRISING THE DEPOSITION OF LAYERS OF MATERIALS IN THE SOLID CONDITION AND / OR FLUID |
US10442523B2 (en) | 2015-08-25 | 2019-10-15 | The Boeing Company | Synergetic noise absorption and anti-icing for aircrafts |
-
2016
- 2016-02-08 GB GB201602240A patent/GB2547049B/en active Active
-
2017
- 2017-02-08 WO PCT/GB2017/050312 patent/WO2017137740A1/en active Application Filing
- 2017-02-08 EP EP17705458.2A patent/EP3414446B1/en active Active
- 2017-02-08 CN CN201780010410.6A patent/CN109072816B/en active Active
- 2017-02-08 US US16/074,442 patent/US11338933B2/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5841079A (en) * | 1997-11-03 | 1998-11-24 | Northrop Grumman Corporation | Combined acoustic and anti-ice engine inlet liner |
EP1845018A2 (en) * | 2006-04-14 | 2007-10-17 | Rohr, Inc. | Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein |
EP2292514A2 (en) * | 2009-09-03 | 2011-03-09 | The Boeing Company | Ice protection system and method |
GB2476855A (en) * | 2009-11-27 | 2011-07-13 | Rolls Royce Plc | Acoustic liner and heat exchanger for gas turbine inlet duct |
WO2014102682A1 (en) * | 2012-12-27 | 2014-07-03 | Alenia Aermacchi S.Pa. | Nacelle for aircraft, provided with a built-in system for anti-icing protection and acoustic absorption |
Also Published As
Publication number | Publication date |
---|---|
EP3414446A1 (en) | 2018-12-19 |
CN109072816B (en) | 2022-03-08 |
US11338933B2 (en) | 2022-05-24 |
US20190039746A1 (en) | 2019-02-07 |
GB2547049A (en) | 2017-08-09 |
CN109072816A (en) | 2018-12-21 |
WO2017137740A1 (en) | 2017-08-17 |
EP3414446B1 (en) | 2024-05-15 |
GB201602240D0 (en) | 2016-03-23 |
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